Fuel Selector Confusion on Climb-Out

Departing Tampa Executive Airport (KVDF), Tampa, FL — Runway 05, climbing out on a 042° heading. Elevation 22 ft MSL. It is a clear, calm morning: OAT 18°C, altimeter 29.98, light winds from 080°. Visibility 10+ SM. A straightforward VFR departure.

You are a Private pilot with 280 hours total time, 45 hours in the Piper Cherokee 180. This is a familiar airplane at a familiar field. You have flown this route a dozen times. You are not distracted — you are heads-down on the climb, monitoring airspeed and heading, scanning the engine instruments.

At 400 ft AGL, climbing through 74 KIAS (Vy, best rate of climb), the engine begins to sputter. The tachometer is unwinding. Power is dropping. You are still over the airport's immediate environment — wooded wetland and pasture to the north, medium development to the west. The runway is still within gliding distance behind you.

Aircraft: Piper Cherokee 180, solo, full fuel (48 gallons total — 24 gallons left tank, 24 gallons right tank). You completed a full preflight, including a visual fuel check in both tanks. The airplane was airworthy at departure. The fuel selector is in the LEFT position — you selected it before engine start and did not move it during the run-up or takeoff roll.

Pilot: You — Private, current, 280 hours total, 45 hours in type. You did not cross-check the fuel selector position against the fuel quantity gauges during the run-up. You did not verify the fuel selector position one final time before takeoff. You are now at 400 ft AGL with a sputtering engine and a decision to make in the next 30 seconds.

NTSB WPR24LA178 (2024): A Piper PA-28 on a personal flight lost engine power due to fuel starvation when the pilot placed the fuel selector in an intermediate position. The probable cause was the pilot's incorrect movement of the fuel selector valve to an off or restricted position. The airplane made a forced landing.

NTSB CEN24LA191 (2024): A Piper PA-28-180 on a cross-country personal flight lost engine power due to fuel starvation when the pilot failed to switch fuel tanks while distracted crossing a mountain range. The probable cause was the pilot's inattention to fuel management procedures. The airplane made a forced landing in a field.

NTSB CEN24LA189 (2024): A Piper PA-28-180 on an instructional flight lost all engine power when the student pilot positioned the fuel selector valve between port positions during descent. The probable cause was the student pilot's improper fuel tank selection. The flight instructor performed a forced landing.

NTSB ERA24LA116 (2024): A Piper PA-28-180 experienced fuel starvation during the second approach to landing after the student pilot failed to switch fuel tanks despite instructor reminders. The probable cause was the student pilot's lack of fuel management and the flight instructor's inadequate monitoring. The airplane made a forced landing on a highway.

NTSB CEN24LA108 (2024): A Piper PA-28 on an instructional flight experienced fuel starvation when the student pilot inadvertently positioned the fuel selector toward the OFF position during a fuel tank change. The probable cause was the student pilot's improper movement of the fuel selector to the OFF position. The flight instructor performed a forced landing to a field.

NTSB DFW05FA028 (2004, FATAL): A Piper PA-28-180 on a Part 91 night cross-country flight lost engine power due to fuel starvation from improper fuel tank management. The pilot failed to switch fuel tank position. The airplane impacted terrain. The probable cause was the pilot's in-flight mismanagement of the available fuel supply by failure to switch fuel tank position.

NTSB MIA02FA144 (2002, FATAL): A Piper PA-28-180 lost engine power on downwind leg shortly after takeoff. The probable cause was the misrouting of the fuel lines to the fuel selector, which resulted in the use of a fuel tank with inadequate fuel supply. The airplane struck trees and terrain.

NTSB NYC03LA096 (2003): A Piper PA-28-180 on an instructional flight experienced partial engine power loss on initial climb after takeoff and made a forced landing in a field. The probable cause was an inadequate 100-hour inspection that failed to detect a loose fuel line connection.

The consistent thread across all these events: the Piper Cherokee 180's LEFT/RIGHT fuel selector is not forgiving. There is no BOTH position. The pilot must actively switch tanks during flight. Running a selected tank dry — or taking off on a nearly empty tank — is the signature starvation trap. The first symptom is often a sputtering engine and a dropping tachometer at low altitude, exactly when there is no time to diagnose and recover.

The real accidents cited above occurred at other airports and in other aircraft — NOT at KVDF. KVDF has its own accident history (see field dominant patterns), but these specific events happened elsewhere. The scenario is localized to KVDF to make the off-field environment real and consequential for you as a student here.

Off Runway 05's departure end, the off-field environment is wooded wetland, pasture, and medium development — all suitable for a forced landing. Off Runway 36's departure end, the off-field environment includes open water — a forced landing off that end is a ditching. Know the terrain before you depart.